Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = '1900C' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = '1900C' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR JIKA2013120301Switch · out of adjustDURING CLIMB OUT AT APPROXIMATELY 12,000 FEET FROM DFW THE FWD CABIN DOOR ANNUNCIATOR ILLUMINATED. THE PILOT PROCEEDED WITH THE EMERGENCY CHECKLIST ITEMS. PILOT DECIDED TO RETURN TO DFW, PILOT DID NOT DECLARE AN EMERGENCY & LANDED WITHOUT INCIDENT. DFW MX ISDR TIMA20131114013Seat Track · corrodedDURING MAINTENANCE INSPECTION THE RT SIDE SEAT SUPPORT RAIL WAS FOUND TO BE CORRODED. SIDE SEAT SUPPORT WAS REPLACED WITH A NEW PART IAW FR CO 101219 REV 1.SDR TIMA20131114012Seat Track · corrodedDURING MAINTENANCE INSPECTION THE LT SIDE SEAT SUPPORT RAIL WAS FOUND TO BE CORRODED. SIDE SEAT SUPPORT WAS REPLACED WITH A NEW PART IAW FR-CO-101219 REV 1.SDR JIKA2013110401Powerpack · leakingDURING APPROACH, PILOT SELECTED GEAR DOWN, AND NOTICE LANDING GEAR INDICATOR DID NOT INDICATE THREE GREEN LIGHTS. PILOT DISCONTINUED APPROACH AND PERFORMED MANUAL GEAR EXTENSION; INDICATOR SHOWED 3 GREEN LIGHTS GEAR DOWN AND LOCKED. PILOT LANDED WITH NO FURTSDR JIKA2013102901Circuit Board · faultyDURING CRUISE, FLIGHT CREW NOTICED THREE GREEN LIGHTS WERE NOT ILLUMINATED AFTER SELECTING GEAR DOWN. FLIGHT CREW TRIED TROUBLESHOOTING SYS, ELECTED TO FOLLOW PROCEDURES FOR MANUAL GEAR EXTENSION. PILOT LANDED WITHOUT FURTHER INCIDENT. AFTER LANDING MAINTSDR CA131007005Engine · power loss(CAN) APPROXIMATELY 30 MIN INTO A FLIGHT, THE POWER STARTED TO GRADUALLY DECREASE. THE PILOT DIVERTED THE FLIGHT AND LANDED SAFELY. POST FLIGHT ENGINE RUN UP RESULTED IN THE ENGINE HANGING AT 38 PERCENT COMPRESSOR SPEED. TROUBLESHOOTING IS ON-GOING.SDR EPUA20130817001Blower Motor · failedELECTRICAL SMOKE ODOR IN COCKPIT. REPLACED FORWARD AND AFT BLOWER MOTORS IAW MM 21-20. OPS CHECK SATISFACTORY. NO ELECTRICAL ODOR OR SMOKE PRESENT.SDR CA130904012Blade · damaged(CAN) DURING THE 50 HOUR INSPECTION ON ACFT, A "BUBBLE" WAS NOTICED ON ONE OF THE LT PROP BLADES. FURTHER INVESTIGATION SHOWED DELAMINATION ON THE PROP BLADE THAT WAS 23" FROM THE BLADE TIP, AND ABOUT 1.320" X 0.745" IN SIZE. THE LT PROP SN IS FWA2835.SDR TIMA20130830009Skin · corrodedCORROSION FOUND ON BELLY OF ACFT UNDER ADF ANTENNA BS 183.25. REPAIRED.SDR TIMA20130818008Fcu · faultyRT ENGINE SLOWLY LOST TORQUE DURING CRUISE AT FL 200. ENGINE TORQUE EVENTUALLY FELL TO 0 AND ENGINE WAS SHUTDOWN. ACFT DIVERTED AND LANDED UNEVENTFULLY. PROBLEM WAS DETERMINED TO BE A FAULTY ENGINE FUEL CONTROL UNIT.SDR ERAA201308010054Support · chafedCHAFE DAMAGE NOTED AT RT MLG KEEL NEAR ACTUATOR HYDRAULIC LINES. REPAIRED IAW FR-CO-100795. OK FOR SERVICE.SDR CA130722003Stop · bent(CAN) WHEN INSTALLING THE REPLACEMENT KIT FOR THE ELEVATOR, BOB WEIGHT STOP ON IT WAS NOTICED THAT THE ACTUAL STOP WAS BENT OVER. THE INSPECTION WAS CARRIED OUT ON THIS COMPONENT ON DECEMBER 18TH, 2011, REF SB 27-3739. DUE TO EMERGENCY AD 2011-27-51, ALL ELSDR CA130705001Sensor · wrong part(CAN) PILOT REPORTED HIS FUEL FEED ANNUNCIATOR ILLUMINATED IN FLIGHT, WHICH WOULD INDICATE THAT ACFT WAS ALMOST OUT OF FUEL. UPON CHECK OF OTHER GAUGES IT WAS FOUND THAT THE FUEL QTY WAS STILL GOOD AND HIS LOW LEVEL FUEL LIGHT WAS EXTINGUISHED, WHICH BOTH THOSSDR CA130628003Terminal · broken(CAN) CREW SELECTED GEAR DOWN FAILED TO GET GEAR DOWN AND LOCKED INDICATION, RECYCLED THE GEAR WITH NO MOVEMENT OF GEAR CONTROL BREAKER POPPED. CREW DEPLOYED THE GEAR WITH EMERGENCY EXTENSION WITH 3 DOWN AND LOCKED INDICATION OBSERVED THE CREW CONTACTED FLIGHSDR CA130626007Gearbox · seized(CAN) AFTER SHUTDOWN FROM A NORMAL FLIGHT (AND SHUTDOWN) IT WAS NOTED THAT THE R/H PROP OF C-GSKM WAS UNABLE TO BE ROTATED. AFTER A MAINTENANCE INVESTIGATION, IT WAS FOUND THAT THE POWER SECTION/REDUCTION GEARBOX WAS SEIZED WHILE THE GAS GENERATOR SECTION OF TSDR TIMA20130617007Rib · crackedTWO CRACKS WERE DISCOVERED IN THE VERTICAL STABILIZER RIB AT CSS 69. REPAIRED IAW SRM 51-10-21.SDR EPUA20130620001Attach Angle · crackedRT AILERON BALANCE WEIGHT ATTACH ANGLE AT RIB STA 42.53 FOUND BROKEN DURING RECURRENT INSPECTION. NO DEFECT NOTED 3000 HRS EARLIER DURING INITIAL INSP REQUIRED BY MSB 27-3928.SDR EPUA20130725001Skin · misinstalledWRINKLES IN BELLY SKIN FORWARD OF CARGO DOOR. FOUND 258 RIVETS NOT INSTALLED ON PREVIOUS SKIN REPLACEMENT. INSTALLED 258 RIVETS IN STRINGERS 11L TO 11R FROM FS 363.25 TO FS 423.25. REINSPECTED ACFT ON 6/27/2013 TO ADDRESS BELLY SKIN IN AFFECTED AREA FOR AN OISDR TIMA20130605006Doubler · crackedA CRACK WAS DISCOVERED IN THE LT HORIZONTAL STABILIZER FWD SPAR DOUBLER. THE LT HORIZONTAL STABILIZER FORWARD SPAR DOUBLER WAS REPLACED WITH A NEW PART.SDR TIMA20130531005Spar Cap · crackedA CRACK WAS DISCOVERED IN THE LT FWD SPAR CAP OF THE VERTICAL STABILIZER ABOVE CSS 61. REPAIRED IAW FR-CO-02599, REV 1.SDR TIMA20130718004Tee Fitting · crackedDURING AN INSPECTION, A CRACK IN THE LT HORIZONTAL STABILIZER LOWER TEE EXTRUSION WAS DISCOVERED. REPAIRED THE CRACKED TEE EXTRUSION BY SPLICING IN A NEW SECTION IAW REPAIR FR-CO-02598. TWO REPAIR ANGLES WERE FABRICATED USING A SECTION OF A NEW TEE.SDR 2013F00122Plunger · out of adjustWHEN THE ACFT REACHED ALTITUDE OF 22,000 FT. THE AFT CARGO DOOR WARNING LIGHT CAME ON. WHEN ACFT DROPPED IN ALTITUDE BELOW 20,000 FT. THE CARGO DOOR WARNING LIGHT EXTINGUISHED. FLIGHT CREW RETURNED TO DEPARTURE AND CALL MX. MX HAD FLIGHT CREW INSPECT CARGO SDR CA130529008Wire · chafed(CAN) ON APPROACH IHAD A DUAL INVERTER FAILURE. IT WAS CONFIRMED THAT THE 26 VAC WIRE WAS SHUTTING OFF THE INVERTERS DUE TO INCREASED RESISTANCE. WIRES X26A20V AND X27A20V (26 VAC FEED LINES) WERE FOUND CHAFFED BEHIND THE CIRCUIT BREAKER PANEL. ALSO FOUND WIRESDR TIMA20130430002Tee Fitting · crackedDURING A SCHEDULED STRUCTURAL INSP A CRACK IN THE LT HORIZONTAL STABILIZER LOWER TEE EXTRUSION WAS DISCOVERED. REPAIRED THE CRACKED TEE EXTRUSION BY SPLICING IN A NEW SECTION OF TEE EXTRUSION IAW FR-CO-02598. 2 REPAIR ANGLES WERE FABRICATED USING A SECTION SDR CA130501004Wire · cracked(CAN) DURING THE L/H ENGINE CHANGE IT WAS NOTED THAT THE TERMINAL END FOR THE PROP DEICE BRUSHES (POWER WIRE) WAS BAD. THE WIRE WAS CUT SO A NEW TERMINAL END COULD BE ATTACHED WHEN IT WAS NOTICED THAT THERE WAS A DEEP CRACK IN THE CASING OF THE POWER WIRE. AFTSDR ERAA20130033Position Switch · faultyRETRACTED LANDING GEAR, GREEN LIGHTS EXTINGUISHED GEAR HANDLE REMAINED ILLUMINATED. REMOVED AND REPLACED NLG UP POSITION SWITCH AND RIGGED IAW B1900C MAINTENANCE MANUAL 32-60-00. PERFORMED GEAR SWING IAW B1900C MAINTENANCE MANUAL 32-30-00. NLG UP POSITION SSDR CA130417003Stringer · corroded(CAN) DURING INSPECTION OF FS 243.25, HEAVY CORROSION WAS DISCOVERED BY MAINTENANCE PERSONNEL. THE CORROSION OCCURRED BETWEEN A STR AND THE OUTER SKIN OF THE FUSELAGE.SDR CA130404003Strut · leaking(CAN) WHILE SKM WAS DOWN FOR REPAIRS IT WAS NOTED THAT THE NLG ASSY, 114-820021-651, WAS LEAKING HYDRAULIC FLUID. UPON FURTHER INVESTIGATION IT WAS FOUND THAT THE BEARING THAT HOLDS THE GT SEAL IN PLACE HAD BEEN EPOXIED IN INSTEAD OF BRAZED. THE FLUID WAS LESDR JIKA2013032301Control Panel · contaminatedPILOT REPORTED THAT ON FINAL APPROACH, GEAR DID NOT COME DOWN WHEN SELECTED, AND NO INDICATIONS OF MOVEMENT (UNSAFE LIGHTS). DECLARED AN EMERGENCY, MANUALLY EXTENDED GEAR AND PERFORMED A TOWER FLY BY TO CONFIRM GEAR WAS DOWN, AND THEN LANDED WITHOUT FURTHER SDR ERAA201303150028Unknown · odorDURING FLIGHT 737 A LOUD BUZZING SOUND IN THE HEADSETS AND SPEAKERS LASTING A COUPLE OF MINUTES. DURING THIS TIME SMELLED HOT ELECTRICAL SMELL. VOLTMETER INDICATING 24 VOLTS. COULD NOT DUPLICATE. CHECKED SPEAKERS OUT, SPEAKERS OKAY. CHECKED AVIONICS OUT ISDR CA130313007Jack · bent(CAN) PRIOR TO LEVELING OFF FOR CRUISE, BOTH PILOTS BEGAN TO HEAR A CLICKING NOISE THROUGH THEIR HEADSETS FOLLOWED BY AN ODOR OF ELECTRICAL BURNING. LT SEAT PILOT REALIZED HE WAS NOT ABLE TO HEAR THROUGH HIS HEADSET. BOTH CREW MEMBERS CHECKED TO SEE IF THEIRSDR ERAA201303010026Gauge · unreliableNR 2 ITT GAUGE UNRELIABLE. REMOVED AND REPLACED NR 2 ENGINE ITT GAUGE. INSPECTED ENGINE WIRING HARNESS AT ENGINE, NO DEFECTS NOTED. OPERATIONAL CHECK GOOD, OK FOR SERVICE AT THIS TIME. REMOVED AND REPLACED IAW BE1900C MM 39-10-00.SDR JIKA2013022101Unknown · malfunctionedON DESCENT INTO KJAC THE PILOT REPORTED THAT HIS LEFT ENGINE POWER LEVER WOULD REDUCE POWER, BUT THERE WAS NO RESPONSE FROM THE LEFT ENGINE WHEN THE PILOT ADVANCED THE LEFT POWER LEVER. THE PILOT SHUT DOWN THE LEFT ENGINE, DECLARED AN EMERGENCY AND LANDED AT SDR CA130225004Oil System · low pressure(CAN) LT ENGINE SUFFERED AN IN-FLIGHT SHUTDOWN DUE TO LOSS OF OIL PRESSURE. THE ACFT RETURNED TO AIRPORT WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAS MADE. TROUBLESHOOTING ONGOING.SDR CA130206002Engine · failed(CAN) ON THE CLIMBOUT AT APPROXIMATELY 7000 FT, THE ACFT EXPERIENCED A SUDDEN RT ENGINE FAILURE. NEITHER FILGHT CREW HAD NOTICED ANY INDICATION OF AN ONCOMING ENGINE PROBLEM PRIOR TO A SUDDEN LOUD POPPING NOISE AND THE ACFT YAWING TO THE RT. THEY INSTANTLY ISDR TIMA20130611001Spar Cap · crackedDURING A SCHEDULED STRUCTURAL INSP A CRACK WAS DISCOVERED IN THE RT FWD SPAR CAP ABOVE CSS 62. REPAIRED CRACK IN FWD RT SPAR CAP BY REMOVING THE DAMAGED SECTION OF THE CAP AND SPLICING IN A NEW SECTION IAW FR-CO-02599.SDR EPUA20130111001Annunciator · faultyLEFT MAIN GEAR SLOW TO SHOW GREEN LIGHT, DOWN AND LOCKED. MX FOUND THAT THE LANDING GEAR ANNUNCIATOR WAS FAULTY. ANNUCIATOR WAS REPLACED. NO FURTHER FAULTS.SDR YADA2013F00016Circuit Breaker · trippedCREW ON FLT 145, DISCOVERED ON APPROACH THAT THE AIRPLANE LANDING GEAR WOULD NOT EXTEND. TOWER WAS NOTIFIED. INITIATED MANUAL GEAR EXTENSION PROCEDURES, WHICH WERE SUCCESSFUL. LANDED WITHOUT INCIDENT. MX FOUND THE 60 AMP LANDING GEAR CIRCUIT BREAKER IN LTSDR CA121231001Relay · failed(CAN) GEAR WAS UNSAFE GOING INTO DESCENT, DIDN`T GET 3 GREEN SO DID AN OVERSHOOT, VFR AND CYCLED THE GEAR IAW CHECKLIST. THE NEXT STEP WAS TO MANUALLY PUMP THE GEAR SO THE CREW OPTED TO GO DIRECT TO THE MAINTENANCE BASE. MAINTENANCE PERSONNEL DISCOVERED THATSDR TIMA201306110011Tee Fitting · crackedDURING A SCHEDULED STRUCTURAL INSPECTION, A CRACK WAS DISCOVERED IN THE LT HORIZONTAL STABILIZER LOWER INBD TEE EXTRUSION. REPAIRED CRACKED TEE EXTRUSION BY SPLICING IN A NEW SECTION IAW FR-CO-02598-1. 2 REPAIR ANGLES, FR-CO-02598-1 WERE FABRICATED FROM A NESDR CA121214003Handle · frozen(CAN) ON ARRIVAL, AFTER SHUTDOWN, THE FLIGHT CREW ATTEMPTED TO OPEN THE MAIN CABIN DOOR BUT THE DOOR HANDLE WAS FROZEN IN POSITION, MAKING IT IMPOSSIBLE FOR THE CREW TO OPEN THE DOOR, OR DISEMBARK THE PASSENGERS. ANOTHER PERSON OUTSIDE THE AIRPLANE HAD TO MOVSDR 2012F00266Bracket · bentAIRCRAFT DEPARTED, ON REACHING AN ALTITUDE OF 20,000 FT THE FORWARD ENTRY DOOR WARNING ANNUNCIATOR ILLUMINATED. THE CREW BURNED OFF EXECESS FUEL AND RETURNED TO BASE. MX PERSONNEL FOUND THE UPPER DOOR AJAR WARNING SWITCH BRACKET WAS BENT. THE BRACKET WAS STSDR CA121207007Mechanism · frozen(CAN) UPON ARRIVAL THE FLIGHT CREW COULD NOT OPEN THE MAIN CABIN DOOR. THE MECHANISM INSIDE THE DOOR WAS FROZEN, SO THE DOOR HANDLE COULD NOT BE TURNED FROM THE INSIDE. A PERSON STANDING OUTSIDE THE AIRCRAFT HAD TO OPERATE THE OUTER DOOR HANDLE IN TANDEM WISDR CA121206011Door · binding(CAN) ON ARRIVAL, AFTER SHUTDOWN THE FLIGHT CREW ATTEMPTED TO OPEN THE MAIN CABIN DOOR, MCD, BUT THE DOOR HANDLE WAS FROZEN IN POSITION, MAKING IT IMPOSSIBLE FOR THE CREW TO OPEN THE DOOR, OR DISEMBARK THE PASSENGERS. PERSON OUTSIDE THE AIRPLANE HAD TO MOVE TSDR EPUA20121212001Shroud · dislodgedDURING DESCENT ON LAST FLIGHT OF DAY, ENGINE TORQUE BEGAN TO DROP OFF. THIS CAUSED THE ACFT TO YAW TO THE RT. ACFT LANDED WITHOUT INCIDENT. MX INSPECTED THE ENGINE AND DETERMINED THAT A COMPRESSOR TURBINE SHROUD SEGMENT HAD BECOME DISLODGED FROM THE SHROUD ASDR HSYA2012113012Wire · brokenPILOT REPORTED DURING A MX CHECK FLIGHT THAT THE GEAR REMAINED DOWN WITH ALL THREE GREEN LIGHTS ILLUMINATED WHEN THE GEAR HANDLE WAS MOVED TO THE UP POSITION. ACFT RETURNED TO DEPARTURE UNEVENTFULLY. MX TROUBLESHOT THE GEAR SYS AND THE FOLLOWING MX WAS PERFOSDR CA121203020Compressor · seized(CAN) DURING SCHEDULED INSPECTION ON THE RT ENGINE, THE AIR CONDITIONING, A/C COMPRESSOR DRIVE BELT WAS FOUND BROKEN WITH SIGNIFICANT HEAT DAMAGE AND SPREAD LIQUID RUBBER THROUGHOUT THE BACK OF THE ENGINE. THIS WAS CAUSED BY THE FAILURE OF THE A/C COMPRESSOR SDR CA121120004Washer · misinstalled(CAN) DURING DISSASSEMBLY AT O/H, IT WAS FOUND THAT THE INTERNAL WASHERS ON THE MAIN ARMATURE SHAFT WERE INSTALLED INCORRECTLY, ALLOWING THE ARMATURE, AND MAIN CONDENSOR BLOWER FAN TO VIBRATE, CAUSING STRUCTURAL DAMAGE TO THE FAN CASE. THIS WAS A NEW PART, PURSDR JDWA719GL002Button · sticksPILOT'S MICROPHONE BUTTON STUCK. PILOT RETURN TO DEPARTURE. MX REPLACED MIC BUTTON.SDR CA121120003Indicator · damaged(CAN) DURING START, THE CREW NOTICED ELECTRICAL BURNING ODOR IN COCKPIT, START ABORTED WITH NO FURTHER PROBLEMS. MAINTENANCE INVESTIGATED AND DISCOVERED THE TCAS/VSI INDICATOR FAILED THE SYS TEST, AND SMELLED OF ELECTRICAL BURNING. TCAS/VSI INDICATOR REPLACE
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